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A peer-reviewed article of this preprint also exists.
This version is not peer-reviewed
Submitted:
24 July 2024
Posted:
25 July 2024
You are already at the latest version
Type of policy tools | example | effect |
Demand-side policy | Public procurement, price subsidies. | Stabilize the market environment for innovation, fostering confidence and stimulating technology research and development. |
Environmental policy | Standard design, goal planning. | Shape product development by setting performance norms, encouraging innovation, and facilitating industry transitions |
Supply-side policy | technology infrastructure, technology input | Support enterprise research and development, encouraging investment and effective resource allocation |
Research and Validation Stage | Early commercialization Stage | Rapid Commercialization Stage | Mature Commercialization Stage | |
Driving mode | Autonomous driving technology awaits validation. | Requiring visual flight conducted by professional pilots in collaboration with assisted driving systems. | The system is responsible for most flight missions, equipped with professional pilots for manual control in emergency situations. | Passenger eVTOL achieve full autonomous flight, overseen remotely by a central control system, removing the requirement for onsite professional pilots. |
Performance | Prototypes need to be explored through continuous experimentation and trial applications | The ideal performance parameters include a range of 150-200 kilometers, a cruising speed of 200-250 kilometers per hour, and a capacity of 4-5 passengers. | The emergence of second and third-generation commercial eVTOL products, and the larger size of eVTOL | A trend towards personalized design, with a variety of eVTOL designed and produced for different speeds, ranges, and appearances |
Air traffic control | \ | Airspace and air traffic control systems have been adapted for low-altitude eVTOL flights, establishing fixed routes. Pre-approval from relevant authorities is required for flight missions. | Airspace management and air traffic control policies are becoming more flexible, with increased automation and shorter flight notification times. | The air traffic management system will be highly efficient, allowing airspace resources to be allocated on demand. |
Infrastructure | \ | Landing and takeoff points are set up near traditional urban transport hubs. | Start spreading to urban commercial and residential centers and expanding into suburban areas. | eVTOL landing and takeoff points are integrated into urban planning. |
Stage | Consumer Groups | New Users | Characteristics |
Research and Validation | Innovators | Technology pioneers, research institutions, aviation enthusiasts | -Interested in emerging technologies and new aircraft -Capable of investing significant resources into research and experimentation -Participate in research and testing processes |
Early Commercialization | Early Adopters | Middle-income travelers, large corporations, affluent private users, individuals in need of air medical and tourism services | -Willing to try new products but more cautious compared to Innovators -Often have substantial incomes |
Rapid Commercialization | Early Majority | Ordinary consumers, urban residents, business travelers | -Majority of consumers -Wait for evidence of reliability and effectiveness -Willing to pay reasonable prices -Concerned about convenience and practicality |
Mature Commercialization | Late Majority and Laggards | Suburban users, conservative individuals | -Cautious about new technologies |
M11 | M12 | M13 | M21 | M22 | M23 | P1 | P2 | P3 | P4 | T1 | T2 | T3 | T4 | G1 | G2 | G3 | G4 | |
M11 | 1 | 1 | 1 | |||||||||||||||
M12 | 1 | 1 | ||||||||||||||||
M13 | ||||||||||||||||||
M21 | 1 | |||||||||||||||||
M22 | 1 | |||||||||||||||||
M23 | ||||||||||||||||||
P1 | 1 | |||||||||||||||||
P2 | 1 | 1 | 1 | |||||||||||||||
P3 | 1 | 1 | 1 | |||||||||||||||
P4 | 1 | 1 | ||||||||||||||||
T1 | 1 | 1 | ||||||||||||||||
T2 | 1 | 1 | 1 | |||||||||||||||
T3 | 1 | 1 | 1 | |||||||||||||||
T4 | 1 | |||||||||||||||||
G1 | 1 | 1 | ||||||||||||||||
G2 | 1 | 1 | ||||||||||||||||
G3 | 1 | 1 | ||||||||||||||||
G4 | 1 | 1 |
M11 | M12 | M13 | M21 | M22 | M23 | P1 | P2 | P3 | P4 | T1 | T2 | T3 | T4 | G1 | G2 | G3 | G4 | |
M11 | 0.444 | 0.235 | 0.444 | 0.235 | 0.333 | 0.259 | ||||||||||||
M12 | 0.444 | 0.111 | 0.333 | |||||||||||||||
M13 | ||||||||||||||||||
M21 | 0.333 | 0.111 | ||||||||||||||||
M22 | 0.333 | |||||||||||||||||
M23 | ||||||||||||||||||
P1 | 0.111 | 0.086 | 0.055 | 0.111 | 0.123 | 0.067 | 0.333 | 0.148 | 0.078 | |||||||||
P2 | 0.333 | 0.259 | 0.165 | 0.333 | 0.370 | 0.202 | 0.444 | 0.235 | ||||||||||
P3 | 0.333 | 0.259 | 0.333 | 0.259 | 0.444 | |||||||||||||
P4 | 0.333 | 0.333 | ||||||||||||||||
T1 | 0.148 | 0.165 | 0.128 | 0.148 | 0.214 | 0.144 | 0.444 | 0.346 | 0.219 | 0.333 | 0.111 | 0.037 | ||||||
T2 | 0.111 | 0.235 | 0.219 | 0.111 | 0.272 | 0.232 | 0.333 | 0.593 | 0.424 | 0.333 | 0.111 | |||||||
T3 | 0.111 | 0.235 | 0.111 | 0.235 | 0.333 | 0.593 | 0.333 | |||||||||||
T4 | 0.111 | 0.111 | 0.333 | |||||||||||||||
G1 | 0.086 | 0.133 | 0.116 | 0.086 | 0.162 | 0.125 | 0.259 | 0.313 | 0.214 | 0.333 | 0.444 | 0.148 | 0.049 | |||||
G2 | 0.037 | 0.115 | 0.151 | 0.037 | 0.128 | 0.155 | 0.111 | 0.309 | 0.339 | 0.333 | 0.444 | 0.148 | ||||||
G3 | 0.111 | 0.198 | 0.111 | 0.198 | 0.333 | 0.481 | ||||||||||||
G4 | 0.333 | 0.444 | 0.148 |
Effect degree (r) | Cause degree (c) | Prominence (r+c) | Relation (r-c) | Weight | |
---|---|---|---|---|---|
M11 | 1.951 | 0.827 | 2.778 | 1.123 | 0.057 |
M12 | 0.889 | 1.993 | 2.882 | -1.104 | 0.059 |
M13 | 0.000 | 2.649 | 2.649 | -2.649 | 0.054 |
M21 | 0.444 | 1.160 | 1.605 | -0.716 | 0.033 |
M22 | 0.333 | 3.047 | 3.380 | -2.713 | 0.069 |
M23 | 0.000 | 3.000 | 3.000 | -3.000 | 0.061 |
P1 | 1.114 | 0.000 | 1.114 | 1.114 | 0.023 |
P2 | 2.342 | 1.481 | 3.823 | 0.860 | 0.078 |
P3 | 1.630 | 3.152 | 4.782 | -1.523 | 0.098 |
P4 | 0.667 | 3.954 | 4.620 | -3.287 | 0.095 |
T1 | 2.439 | 0.333 | 2.772 | 2.105 | 0.057 |
T2 | 2.974 | 1.111 | 4.085 | 1.863 | 0.084 |
T3 | 1.951 | 1.037 | 2.988 | 0.914 | 0.061 |
T4 | 0.556 | 0.679 | 1.235 | -0.123 | 0.025 |
G1 | 2.471 | 0.000 | 2.471 | 2.471 | 0.051 |
G2 | 2.308 | 0.000 | 2.308 | 2.308 | 0.047 |
G3 | 1.432 | 0.000 | 1.432 | 1.432 | 0.029 |
G4 | 0.926 | 0.000 | 0.926 | 0.926 | 0.019 |
Aspect | Strategies |
---|---|
Technical Feasibility | - Develop advanced electric flight technology, including high-energy-density batteries, efficient electric motors, and intelligent power management systems. - Research and deploy infrastructure for flexible takeoff and landing . - Ensure sufficient flight range and passenger capacity. |
Safety | - Implement advanced automatic flight systems, including automatic takeoff and landing, obstacle detection and avoidance, and flight path planning. - Enhance emergency handling capabilities, such as automatic switching to backup power and emergency landing procedures. |
Affordability | - Reduce manufacturing and operating costs through improvements in materials, production processes, scale production, and supply chain management. - Realize and apply fully automatic flight to minimize training and employment costs for professional pilots. - Ensure price competitiveness to attract mainstream customers’ purchases. |
Governmental Policies | - Strategically direct policy support towards facilitating the crossing of the chasm. - Overcome obstacles and streamline policy guidance and support for eVTOL to foster low-altitude economy development. |
Research and Validation | Early Commercialization | Rapid Commercialization | Mature Commercialization | |
Distributed Electric Propulsion | In a period of Strategic opportunities, Most tech inherited from NEV. |
Enhance efficiency, cutting energy use, and reducing emissions. | As the industry chain improves, electric propulsion system production costs will decrease gradually. | Enhance efficiency, manage costs, and incorporate intelligent automation |
Low Aerodynamic Noise Technology | Reducing aircraft noise during takeoff, landing, and flight. | Optimizing multiple goals like noise reduction, energy efficiency, and emissions reduction | Achieve “Low Noise” or even “Zero Noise”, reduce cost | Reach the max limit, aligning with environmental sustainability goals. |
Flight Control Technology | Primarily human-controlled with program assistance. | Primarily program-controlled with human assistance, The flight process is predominantly automated | Enable advanced autonomous operations, cooperative flight and remote control | Utilizing advanced technologies to create a global autonomous driving network |
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